US4832734A - Hot working aluminum-base alloys - Google Patents

Hot working aluminum-base alloys Download PDF

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Publication number
US4832734A
US4832734A US07/190,714 US19071488A US4832734A US 4832734 A US4832734 A US 4832734A US 19071488 A US19071488 A US 19071488A US 4832734 A US4832734 A US 4832734A
Authority
US
United States
Prior art keywords
aluminum
hot working
matrix
volume percent
alloys
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US07/190,714
Other languages
English (en)
Inventor
Raymond C. Benn
Prakash K. Mirchandani
Walter E. Mattson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Huntington Alloys Corp
Original Assignee
Inco Alloys International Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Inco Alloys International Inc filed Critical Inco Alloys International Inc
Assigned to INCO ALLOYS INTERNATIONAL, INC., A CORP. OF DE reassignment INCO ALLOYS INTERNATIONAL, INC., A CORP. OF DE ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: BENN, RAYMOND C., MATTSON, WALTER E., MIRCHANDANI, PRAKASH K.
Priority to US07/190,714 priority Critical patent/US4832734A/en
Priority to JP1107123A priority patent/JPH01316442A/ja
Priority to AU33792/89A priority patent/AU601939B2/en
Priority to KR1019890005799A priority patent/KR920001612B1/ko
Priority to BR898902090A priority patent/BR8902090A/pt
Priority to DE8989108154T priority patent/DE68905652T2/de
Priority to EP89108154A priority patent/EP0340789B1/en
Publication of US4832734A publication Critical patent/US4832734A/en
Application granted granted Critical
Assigned to HUNTINGTON ALLOYS CORPORATION reassignment HUNTINGTON ALLOYS CORPORATION RELEASE OF SECURITY INTEREST Assignors: CREDIT LYONNAIS, NEW YORK BRANCH, AS AGENT
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/14Both compacting and sintering simultaneously
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0052Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides

Definitions

  • the present invention is concerned with hot working of aluminum-base alloys and, more particularly, with hot working by forging, rolling and the like aluminum-base alloys having an ultra-fine hard dispersed transition-metal-intermetallic phase in the microstructure, this intermetallic dispersed phase being of such a character that it cannot be solubilized in the aluminum matrix below the melting point of the matrix.
  • k is an empirical constant (whose value depends upon the characteristics of the matrix alloy), and f is the volume fraction of the hard phase. The above relationship has been shown to hold approximately true at room temperature for a variety of dual or multi-phase alloys, including Al-SiC composites.
  • alloys prepared by mechanical alloying and containing 5-35 volume percent Al 3 Ti in an aluminum matrix along with dispersed Al 4 C 3 and Al 2 O 3 have tensile elongations in excess of 5% and are therefor amenable to hot working.
  • This object also includes the hot worked alloy product.
  • the present invention contemplates hot working by a process permitting metal flow in at least two directions, a mechanically alloyed aluminum-base alloy consisting essentially of an aluminum matrix containing optional solid solution hardeners, about 5 to about 35 volume percent of an aluminum transition metal intermetallic compound, carbide phases, principally aluminum carbide up to about 14 volume percent and optional oxidic phases, principally aluminum oxide up to about 5 volume percent, said hot working being conducted in the temperature interval between 370° C. and the solidus temperature of the aluminum matrix.
  • the invention also contemplates the resultant hot worked alloy which exhibits a unique combination of strength, modulus, ductility and stability over a range of temperatures up to about 95% of the melting temperature (0.95 Tm).
  • the aluminum-base alloys to be hot worked in accordance with the present invention are made by mechanical alloying following generally procedures as described in U.S. Pat. Nos. 3,740,210, 4,668,470 and 4,688,282 using stearic acid as a process control agent.
  • the levels of carbide and oxide set forth in the preceding paragraph generally derive from the levels of process control agent normally used in mechanical alloying with or without intentional inclusion of oxide, e.g. alumina or yttria or carbon in a mechanically alloyed charge.
  • oxide e.g. alumina or yttria or carbon
  • up to about 5 volume percent carbide and 2 volume percent oxide are the usual amounts of these phases encountered when stearic acid is employed as the process control agent with no other non-metallic additions to the charge.
  • compositions of hot worked aluminum-base alloys are set forth in Table 1.
  • the alloys in Table 1 contain roughly 15 to 31 volume percent of aluminum transition metal intermetallic phase, specifically in alloys 1-3 and 11 the phase being Al 3 Ti in the range of 15 to 31 volume percent.
  • the intermetallic phase is a combination made up principally of Al 3 Ti along with aluminides and/or other compounds of other transition metals.
  • the "intermetallic phase” may be a single phase or more than one phase, no specific limitation being implied by the singularity of the term "intermetallic phase”.
  • solid solution hardeners in an aluminum matrix includes not only normal elements such as silicon, copper, lithium, magnesium and zinc which, in conventional amounts, are soluble in a solid aluminum matrix but also those elements which, although forming insoluble products at low temperature, e.g. below 100° C. are soluble in the matrix at the temperature of hot working.
  • carbide phases includes not only aluminum carbide but also titanium carbide, carbides of other alloy ingredients and chemical modifications of aluminum, titanium and other carbides.
  • oxidic phase is intended to include not only aluminum oxide formed by reaction between aluminum and oxygen in the stearic acid process control agent during mechanical alloying but also small amounts, e.g. up to about 5 volume percent of other oxide, e.g. yttria, yttrium-aluminum-garnet or alumina which might be added to or formed while processing a mechanical alloying charge.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Metal Rolling (AREA)
US07/190,714 1988-05-06 1988-05-06 Hot working aluminum-base alloys Expired - Fee Related US4832734A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US07/190,714 US4832734A (en) 1988-05-06 1988-05-06 Hot working aluminum-base alloys
JP1107123A JPH01316442A (ja) 1988-05-06 1989-04-26 熱間加工性アルミニウム基合金
AU33792/89A AU601939B2 (en) 1988-05-06 1989-04-27 Hot working aluminium-base alloys
KR1019890005799A KR920001612B1 (ko) 1988-05-06 1989-05-01 고온가공에 적합한 알루미늄-기초 합금
BR898902090A BR8902090A (pt) 1988-05-06 1989-05-04 Conformacao a quente e artigo conformado a quente
DE8989108154T DE68905652T2 (de) 1988-05-06 1989-05-05 Warmformgebung von aluminiumlegierungen.
EP89108154A EP0340789B1 (en) 1988-05-06 1989-05-05 Hot working aluminum base alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/190,714 US4832734A (en) 1988-05-06 1988-05-06 Hot working aluminum-base alloys

Publications (1)

Publication Number Publication Date
US4832734A true US4832734A (en) 1989-05-23

Family

ID=22702455

Family Applications (1)

Application Number Title Priority Date Filing Date
US07/190,714 Expired - Fee Related US4832734A (en) 1988-05-06 1988-05-06 Hot working aluminum-base alloys

Country Status (7)

Country Link
US (1) US4832734A (ja)
EP (1) EP0340789B1 (ja)
JP (1) JPH01316442A (ja)
KR (1) KR920001612B1 (ja)
AU (1) AU601939B2 (ja)
BR (1) BR8902090A (ja)
DE (1) DE68905652T2 (ja)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4933007A (en) * 1988-10-21 1990-06-12 Showa Aluminum Heat-resistant aluminum-base composites and process of making same
EP0427492A1 (en) * 1989-11-06 1991-05-15 Inco Alloys International, Inc. Aluminum-base composite alloy
GB2248629A (en) * 1990-09-20 1992-04-15 Daido Metal Co Sliding material
US20030056928A1 (en) * 2000-03-13 2003-03-27 Takashi Kubota Method for producing composite material and composite material produced thereby
CN110964951A (zh) * 2019-12-27 2020-04-07 成都航空职业技术学院 一种Fe-C-Ti/ZL108复合材料及其制备方法

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5169461A (en) * 1990-11-19 1992-12-08 Inco Alloys International, Inc. High temperature aluminum-base alloy
US5171381A (en) * 1991-02-28 1992-12-15 Inco Alloys International, Inc. Intermediate temperature aluminum-base alloy

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3740210A (en) * 1971-07-06 1973-06-19 Int Nickel Co Mechanically alloyed aluminum aluminum oxide
US3874938A (en) * 1971-04-06 1975-04-01 Int Nickel Co Hot working of dispersion-strengthened heat resistant alloys and the product thereof
US4292079A (en) * 1978-10-16 1981-09-29 The International Nickel Co., Inc. High strength aluminum alloy and process
US4297136A (en) * 1978-10-16 1981-10-27 The International Nickel Co., Inc. High strength aluminum alloy and process
US4600556A (en) * 1983-08-08 1986-07-15 Inco Alloys International, Inc. Dispersion strengthened mechanically alloyed Al-Mg-Li
US4624705A (en) * 1986-04-04 1986-11-25 Inco Alloys International, Inc. Mechanical alloying
US4668282A (en) * 1985-12-16 1987-05-26 Inco Alloys International, Inc. Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US4668470A (en) * 1985-12-16 1987-05-26 Inco Alloys International, Inc. Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US4688282A (en) 1986-07-29 1987-08-25 Jeffries Deidra B Bedding for children
US4722751A (en) * 1983-12-19 1988-02-02 Sumitomo Electric Industries, Ltd. Dispersion-strengthened heat- and wear-resistant aluminum alloy and process for producing same

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
JPS60131943A (ja) * 1983-12-19 1985-07-13 Sumitomo Electric Ind Ltd 分散粒子強化耐熱耐摩耗アルミニウム合金粉末
JPS60131944A (ja) * 1983-12-19 1985-07-13 Sumitomo Electric Ind Ltd 超耐熱耐摩耗アルミニウム合金およびその製造用複合粉末

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3874938A (en) * 1971-04-06 1975-04-01 Int Nickel Co Hot working of dispersion-strengthened heat resistant alloys and the product thereof
US3740210A (en) * 1971-07-06 1973-06-19 Int Nickel Co Mechanically alloyed aluminum aluminum oxide
US4292079A (en) * 1978-10-16 1981-09-29 The International Nickel Co., Inc. High strength aluminum alloy and process
US4297136A (en) * 1978-10-16 1981-10-27 The International Nickel Co., Inc. High strength aluminum alloy and process
US4600556A (en) * 1983-08-08 1986-07-15 Inco Alloys International, Inc. Dispersion strengthened mechanically alloyed Al-Mg-Li
US4722751A (en) * 1983-12-19 1988-02-02 Sumitomo Electric Industries, Ltd. Dispersion-strengthened heat- and wear-resistant aluminum alloy and process for producing same
US4668282A (en) * 1985-12-16 1987-05-26 Inco Alloys International, Inc. Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US4668470A (en) * 1985-12-16 1987-05-26 Inco Alloys International, Inc. Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US4624705A (en) * 1986-04-04 1986-11-25 Inco Alloys International, Inc. Mechanical alloying
US4688282A (en) 1986-07-29 1987-08-25 Jeffries Deidra B Bedding for children

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
Quarterly Report No. 01 900 F. Al Maters. Research Air Force Cont. No. F 33615 86 C 6074, Oct. 1986, pages cover, Legend II. *
Quarterly Report No. 01 900°F. Al Maters. Research Air Force Cont. No. F 33615-86-C-6074, Oct. 1986, pages cover, Legend II.
W.A.L. Tech. Report AFML TR 79 4210. *
W.A.L. Tech. Report AFML-TR 79-4210.

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4933007A (en) * 1988-10-21 1990-06-12 Showa Aluminum Heat-resistant aluminum-base composites and process of making same
EP0427492A1 (en) * 1989-11-06 1991-05-15 Inco Alloys International, Inc. Aluminum-base composite alloy
US5114505A (en) * 1989-11-06 1992-05-19 Inco Alloys International, Inc. Aluminum-base composite alloy
GB2248629A (en) * 1990-09-20 1992-04-15 Daido Metal Co Sliding material
US5128213A (en) * 1990-09-20 1992-07-07 Daido Metal Company Limited Sliding material of single substance and composite sliding material
GB2248629B (en) * 1990-09-20 1995-03-29 Daido Metal Co Sliding material
US20030056928A1 (en) * 2000-03-13 2003-03-27 Takashi Kubota Method for producing composite material and composite material produced thereby
CN110964951A (zh) * 2019-12-27 2020-04-07 成都航空职业技术学院 一种Fe-C-Ti/ZL108复合材料及其制备方法

Also Published As

Publication number Publication date
BR8902090A (pt) 1989-12-05
DE68905652D1 (de) 1993-05-06
EP0340789B1 (en) 1993-03-31
EP0340789A1 (en) 1989-11-08
AU3379289A (en) 1989-11-09
JPH01316442A (ja) 1989-12-21
DE68905652T2 (de) 1993-07-15
KR890017376A (ko) 1989-12-15
AU601939B2 (en) 1990-09-20
KR920001612B1 (ko) 1992-02-20

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Legal Events

Date Code Title Description
AS Assignment

Owner name: INCO ALLOYS INTERNATIONAL, INC., A CORP. OF DE,WES

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:BENN, RAYMOND C.;MIRCHANDANI, PRAKASH K.;MATTSON, WALTER E.;REEL/FRAME:004882/0049

Effective date: 19880429

Owner name: INCO ALLOYS INTERNATIONAL, INC., HUNTINGTON, WEST

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNORS:BENN, RAYMOND C.;MIRCHANDANI, PRAKASH K.;MATTSON, WALTER E.;REEL/FRAME:004882/0049

Effective date: 19880429

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Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

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LAPS Lapse for failure to pay maintenance fees
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Effective date: 20010523

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Owner name: HUNTINGTON ALLOYS CORPORATION, WEST VIRGINIA

Free format text: RELEASE OF SECURITY INTEREST;ASSIGNOR:CREDIT LYONNAIS, NEW YORK BRANCH, AS AGENT;REEL/FRAME:014863/0704

Effective date: 20031126

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362